WO2017127091A1 - Contrôleur à jeu d'instructions réduit pour capteur de lacunes d'azote de diamant - Google Patents

Contrôleur à jeu d'instructions réduit pour capteur de lacunes d'azote de diamant Download PDF

Info

Publication number
WO2017127091A1
WO2017127091A1 PCT/US2016/014376 US2016014376W WO2017127091A1 WO 2017127091 A1 WO2017127091 A1 WO 2017127091A1 US 2016014376 W US2016014376 W US 2016014376W WO 2017127091 A1 WO2017127091 A1 WO 2017127091A1
Authority
WO
WIPO (PCT)
Prior art keywords
controller
digital control
waveform generator
waveform
single chip
Prior art date
Application number
PCT/US2016/014376
Other languages
English (en)
Inventor
David N. Coar
Jon C. Russo
Boris Shishkin
Original Assignee
Lockheed Martin Corporation
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Lockheed Martin Corporation filed Critical Lockheed Martin Corporation
Publication of WO2017127091A1 publication Critical patent/WO2017127091A1/fr

Links

Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01RMEASURING ELECTRIC VARIABLES; MEASURING MAGNETIC VARIABLES
    • G01R33/00Arrangements or instruments for measuring magnetic variables
    • G01R33/02Measuring direction or magnitude of magnetic fields or magnetic flux
    • G01R33/032Measuring direction or magnitude of magnetic fields or magnetic flux using magneto-optic devices, e.g. Faraday or Cotton-Mouton effect
    • GPHYSICS
    • G05CONTROLLING; REGULATING
    • G05BCONTROL OR REGULATING SYSTEMS IN GENERAL; FUNCTIONAL ELEMENTS OF SUCH SYSTEMS; MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS OR ELEMENTS
    • G05B19/00Programme-control systems
    • G05B19/02Programme-control systems electric
    • G05B19/04Programme control other than numerical control, i.e. in sequence controllers or logic controllers
    • GPHYSICS
    • G05CONTROLLING; REGULATING
    • G05BCONTROL OR REGULATING SYSTEMS IN GENERAL; FUNCTIONAL ELEMENTS OF SUCH SYSTEMS; MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS OR ELEMENTS
    • G05B19/00Programme-control systems
    • G05B19/02Programme-control systems electric
    • G05B19/04Programme control other than numerical control, i.e. in sequence controllers or logic controllers
    • G05B19/042Programme control other than numerical control, i.e. in sequence controllers or logic controllers using digital processors
    • GPHYSICS
    • G05CONTROLLING; REGULATING
    • G05BCONTROL OR REGULATING SYSTEMS IN GENERAL; FUNCTIONAL ELEMENTS OF SUCH SYSTEMS; MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS OR ELEMENTS
    • G05B2219/00Program-control systems
    • G05B2219/20Pc systems
    • G05B2219/25Pc structure of the system
    • G05B2219/25126Synchronize communication based on internal clock of microprocessor

Definitions

  • the subject technology generally relates to magnetometry, and more particularly, to synchronous control, radio-frequency (RF) synthesis, and fluorescence acquisition processor for diamond nitrogen-vacancy (DNV).
  • RF radio-frequency
  • DNV diamond nitrogen-vacancy
  • Atomic-sized nitrogen-vacancy (NV) centers in diamond lattices have been shown to have excellent sensitivity for magnetic field measurement and enable fabrication of small magnetic sensors that can readily replace existing-technology (e.g., Hall-effect) systems and devices.
  • the diamond NV (DNV) sensors are maintained in room temperature and atmospheric pressure and can be even used in liquid environments.
  • a green optical source e.g., a laser or a micro-LED
  • the distance between the two spin resonance frequencies is a measure of the strength of the external magnetic field.
  • a photo detector can measure the fluorescence (red light) emitted by the optically excited NV centers and a DNV system is used to control the laser and microwave timings and perform the data acquisition.
  • One implementation relates to a controller for a DNV sensor that includes a RF waveform generator for generating a RF waveform for a RF signal for a DNV sensor and a digital control for controlling a laser for the DNV sensor.
  • the RF waveform generator and the digital control are formed in a single chip.
  • the single chip is a field-programmable gate array or an application specific integrated circuit.
  • the RF waveform generator and the digital control operate on single-cycle instructions or two-cycle instructions.
  • the RF waveform generator and the digital control operate on single-cycle instructions of a reduced instruction set.
  • the RF waveform generator includes a coordinate rotation digital computer.
  • the RF waveform generator utilizes a frequency base and a frequency increment to generate the RF waveform.
  • the RF waveform generated by the RF waveform generator is processed through an upconverter to generate the RF signal.
  • the digital control includes RF gating.
  • the digital control includes general inputs or outputs. In some implementations, the digital control is configured to control the generation of the RF waveform. In some implementations, the digital control is configured to control optic pulsing of the laser. In some implementations, the single chip is configured to be integrated into one of a geo-location system, an anomaly detection system, a distributed measure point system, a communication system, an unmanned air vehicle, a micro unmanned air vehicle, a missile, an unmanned sea vehicle, an unmanned underground vehicle, or a satellite.
  • Another implementation relates to a controller for a DNV sensor that includes a RF waveform generator for generating a RF waveform for a RF signal for a DNV sensor, a digital control for controlling a laser for the DNV sensor, and an acquisition processor.
  • the RF waveform generator, the digital control, and the acquisition processor are formed in a single chip.
  • the single chip is a field-programmable gate array or an application specific integrated circuit.
  • the RF waveform generator, the digital control, and the acquisition processor operate on single-cycle instructions or two-cycle instructions.
  • the RF waveform generator, the digital control, and the acquisition processor operate on single-cycle instructions of a reduced instruction set.
  • the acquisition processor preprocesses data received from a photo detector of the DNV sensor.
  • the acquisition processor decimates the data received from the photo detector of the DNV sensor.
  • the single chip is configured to be integrated into one of a geo-location system, an anomaly detection system, a distributed measure point system, a communication system, an unmanned air vehicle, a micro unmanned air vehicle, a missile, an unmanned sea vehicle, an unmanned underground vehicle, or a satellite.
  • Yet another implementation relates to a controller for a DNV sensor that includes a RF waveform generator for generating a RF waveform for a RF signal for a DNV sensor, a digital control for controlling a laser for the DNV sensor, an acquisition processor, a host interface for interfacing with an external system, a program counter, a program memory, and a jump control.
  • the the RF waveform generator, the digital control, the acquisition processor, the host interface, the program counter, the program memory, and the jump control are formed in a single chip
  • the single chip is a field-programmable gate array or an application specific integrated circuit.
  • the RF waveform generator, the digital control, and the acquisition processor operate on single-cycle instructions or two-cycle instructions.
  • the RF waveform generator, the digital control, and the acquisition processor operate on single-cycle instructions of a reduced instruction set.
  • the single chip is configured to be integrated into one of a geo-location system, an anomaly detection system, a distributed measure point system, a communication system, an unmanned air vehicle, a micro unmanned air vehicle, a missile, an unmanned sea vehicle, an unmanned underground vehicle, or a satellite.
  • FIG. 1 is a block diagram of an overview of a single-cycle synthesis, control, and acquisition system for a diamond nitrogen vacancy sensor
  • FIG. 2 is a block circuit diagram of the single-cycle control, synthesis, and acquisition processor for a diamond nitrogen vacancy sensor of FIG. 1;
  • FIG. 3 A is a block circuit diagram of the host interface of FIG. 2;
  • FIG. 3B is a block circuit diagram of the program counter of FIG. 2;
  • FIG. 3C is a block circuit diagram of the program memory of FIG. 2;
  • FIG. 3D is a block circuit diagram of a first portion of the jump control with delay of
  • FIG. 2
  • FIG. 3E is a block circuit diagram of a second portion of the jump control FIG. 2;
  • FIG. 3F is a block circuit diagram of the RF waveform generator of FIG. 2;
  • FIG. 3G is a block circuit diagram of the digital control of FIG. 2;
  • FIG. 3H is a block circuit diagram of the acquisition processor of FIG. 2;
  • FIG. 4 is a block diagram depicting a general architecture for a computer system that may be employed to interact various elements of the systems and methods described and illustrated herein.
  • the disclosed system includes a reduced instruction set (RISC) processor that is coupled to a configurable signal synthesizer.
  • RISC reduced instruction set
  • the configurable signal synthesizer may be configured to perform single-cycle commands for frequency shifts, digital outputs, and initial synchronous preprocessing of received data such that the digital control, acquisition, and waveform generation may be performed on the same clock cycle for synchronization.
  • the specially designed single-cycle operations of the subject technology may provide more precise and deterministic timing for digital control, acquisition, and waveform generation.
  • the RF waveform generation and digital control outputs are coordinated in configurable patterns that can range from simple sequences to complex adaptive control patterns.
  • FIG. 1 is a block diagram depicting an overview of an implementation of a single-cycle synthesis, control, and acquisition system 100.
  • the system 100 is configured to control multiple RF signals and digital output signals for magnetometry, such as for a diamond nitrogen vacancy (DNV) sensor.
  • the system 100 may be implemented as a field- programmable gate array (FPGA) or may be implemented as an application specific integrated circuit (ASIC).
  • FPGA field- programmable gate array
  • ASIC application specific integrated circuit
  • the system 100 is implemented as a single single-cycle integrated circuit for RF waveform synthesis, digital control, and acquisition.
  • a more detailed implementation of the single-cycle synthesis, control, and acquisition system is shown as the system 200 in FIG. 2.
  • the system 100 includes a host interface 110 that receives DNV sensing information from an external system, such as a data processing or acquisition system (not shown), and is communicatively coupled to a program counter 120, a program memory 130, and an acquisition processor 180.
  • the host interface 110 may be coupled to a data processing system, such as system 300 of FIG. 3, that can communicate with the system 100 via the host interface 110.
  • the data processing system can output instructions, such as control instructions from the reduced instruction set, to the system 100 via the host interface 110 for the program memory 130.
  • the data acquisition system can also receive output from the acquisition processor 180 via the host interface 110, such as pulse processed data from a DNV sensor.
  • the host interface 110 provides communication between the components of the system 100 and an external system.
  • a more detailed depiction of the host interface 110 is shown as host interface 210 in FIGS. 2 and 3 A.
  • the host interface 110 is communicatively coupled to the program counter 120, which is in communication with the program memory 130 and thejump control 170.
  • a more detailed implementation of the program counter 120 is shown as program counter 220 in FIGS. 2 and 3B.
  • a more detailed implementation of the program memory 130 is shown as program memory 230a, 230b in FIGS. 2 and 3C.
  • a more detailed implementation of thejump control 170 is shown as jump control with delay 240a and the jump control 240b in FIGS. 2 and 3D-E.
  • the program memory 130 provides outputs through a decoder 140 to a RF waveform generator of the
  • CORDIC Coordinat Rotation Digital Computer
  • the CORDIC synthesis 150 provides digital up or down conversion and can have a runtime configurable base frequency and increment for the RF waveform generation.
  • the RF waveform generator of the CORDIC synthesis 150 utilizes a frequency base value and a frequency increment that outputs a single value for a slope of a ramp that is used by an accumulator to generate a sine wave for the RF waveform.
  • the sine wave is processed through an upconverter to generate the RF waveform signal to be applied to the magnetometry component, such as a DNV sensor.
  • the CORDIC synthesis 150 may phase shift the RF waveform. For instance, an analog or digital switch may be used for arbitrary waveform generation.
  • a more detailed implementation of the RF waveform generator and CORDIC synthesis 150 is shown as RF waveform generator 250 in FIGS. 2 and 3F.
  • the digital control 150 provides timing control for a number of aspects of a
  • the digital control 150 includes RF gating or switches and may include additional general inputs or outputs for additional control.
  • the digital control 150 may output signals to control the activation of a magnetometry component, such as a laser for exciting a nitrogen vacancies of a DNV sensor.
  • the digital control can also convert the CORDIC output to 0 via a multiplexer (MUX) such that no RF signal is applied to the DNV sensor.
  • MUX multiplexer
  • the digital control 150 can be used for an acousto-optic modulator (AOM) to control optic pulsing of the laser and/or can be used for phase shift control.
  • the digital control 150 may further provide an output to an I/Q component, such as a digital I/Q.
  • a more detailed implementation of the digital control 160 is shown as digital control 260 in FIGS. 2 and 3G.
  • the acquisition processor 180 provides initial synchronous preprocessing of data received from a magnetometry component, such as data received from a photo detector of a DNV sensor.
  • the acquisition processor 180 can include two coherent channels for simultaneous collection of data, such as the collection of red light, infrared, laser, etc. data. In some implementations, the channels may be chainable up to four. In an implementation with a photo detector, data received by the acquisition processor 180 may be at a rate of 50 MHz, 100 MHz, 200 MHz, or greater. To reduce the amount of data transferred to an external system from the system 100, the acquisition processor can preprocess the data to reduce the size of the data outputted.
  • the acquisition processor 180 synchronously gathers samples from a magnetometry component, such as the photo detector of a DNV sensor, and preprocesses the data, such as decimation of the data.
  • the acquisition process 180 may include a digital output to trigger an accumulator for a predetermined number of clock cycles and then will subtract from two integration windows for processing of the data.
  • the acquisition processor 180 may include a digitally controllable offset for effects similar to a DC block or AC coupling. A more detailed implementation of the acquisition processor 180 is shown as acquisition processor 270 in FIGS. 2 and 3H.
  • the system 100 is configured for single-cycle instructions for the components of the system 100 such that the RF waveform generator of the CORDIC synthesis 150 for generating the RF waveform, the digital control 160 for controlling the laser on/off timing, and the acquisition processor 180 operate on the same clock cycle.
  • a main counter (not shown) drives the RF waveform generation while the program counter 120 allows for delays to be implemented for the digital control 150 and the acquisition processor 180.
  • the single-cycle can provide laser and/or microwave deterministic timing control for coordination of the
  • the single-cycle tightly ties in the digital control 160 for controlling the laser and acquisition processor with the RF waveform generation of the CORDIC synthesis 150.
  • the single-cycle permits synchronous stepped-frequency complex waveform synthesis by the CORDIC synthesis 150 and permits coordinated large-range frequency retuning (e.g., >1 GHz) without losing base time.
  • the single-cycle system 100 can also provide synchronous reduced instruction set program control of the frequency for the RF waveform synthesis.
  • the system 100 of FIG. 1 with a single- cycle also reduces redundant components compared to systems that utilize separate components for the RF waveform generator, digital control, and/or acquisition processor. In some
  • the single-cycle synthesis, control, and acquisition system 100 may also be configured for two-cycle implementations as well.
  • the system 100 can utilize a reduced instruction set (RISC) engine that issues one instruction per clock cycle, including for conditional branching.
  • the reduced instruction set can include commands for an unconditional jump (jmp), a conditional jump (cjmp), setting of a loop counter (setc ⁇ counter value>), setting of a frequency (set/ value>), setting of a digital control output field (seto ⁇ output field value>), a frequency increment (incf ⁇ increment value>), and a delay for a specified cycle count (del ⁇ cycle count value>).
  • the single-cycle synthesis, control, and acquisition system 100 can provide lock-step precision for laser on/off timing via the digital control 160, sequenced microwave waveform synthesis and delivery via the RF waveform generator and CORDIC synthesis 150, data acquisition via the acquisition processor 170, and laser and /or microwave deterministic timing control.
  • the single-cycle synthesis, control, and acquisition system 100 can facilitate effective experimentation by enabling rapid coordination of excitation signals and tuning across broad frequency ranges without losing timing.
  • Not all of the depicted components may be required, however, and one or more implementations may include additional components not shown in the figure. Variations in the arrangement and type of the components may be made, and additional components, different components, or fewer components may be provided.
  • FIG. 2 is a circuit diagram illustrating an example implementation of the single-cycle synthesis, control, and acquisition system 200.
  • the single-cycle synthesis, control, and acquisition system 200 as implemented by the circuit of FIG. 2, is a dedicated hardware configured for DNV applications that are customized to the unique requirements of controlling multiple, diverse instruments and sensors across the RF to optical domain.
  • the reduced instruction set (RISC) engine is configured to issue one instruction per clock cycle, even for conditional branches.
  • the RF waveform generator uses a run-time configurable base frequency and increment to provide the CORDIC synthesis with an RF waveform for digital up/down conversion.
  • the digital control block is responsible for providing laser timing, RF gating, and additional general control input/output (I/O).
  • the acquisition processor block is configured to provide two coherent channels (potentially chainable up to 4) for simultaneous red, infra-red (IR), laser, and other types of light collection.
  • the acquisition processing block is further configured to synchronously collect samples and to provide digitally controllable analog offset that allows effects like DC blocking or AC coupling.
  • Examples of advantageous features of the single-cycle synthesis, control, and acquisition system 200 include, but are not limited to, single-cycle deterministic timing coordination of RF waveform generation, laser control, and data acquisition, synchronous stepped-frequency for complex waveform synthesis, synchronous RISC program control of frequency, coordinated large-range (e.g., >lGHz) frequency retuning without losing time base, and a minimal instruction set.
  • the system 100, 200 can be incorporated into a variety of settings and configurations where DNV magnetometers are employed.
  • Examples of applications of the single-cycle synthesis, control, and acquisition system 100, 200 include, but are not limited to incorporating the single chip into a DNV sensor, incorporating the single chip into DNV-based geolocation systems, incorporating the single chip into DNV anomaly detection systems, incorporating the single chip into covert communications systems, incorporating the single chip into distributed measure point systems, incorporating the single chip into small form factor unmanned systems for air (e.g., unmanned air vehicle (UAV), micro unmanned air vehicle ( ⁇ ), missiles), sea, underground, and surveillance (e.g., satellites, cluster satellites, etc.), incorporating the single chip into low SWAP (size, weight, and power) applications, and utilizing the single chip, single-cycle synthesis, control, and acquisition system 100, 200 for automatic experimental optimization.
  • UAV unmanned air vehicle
  • micro unmanned air vehicle
  • missiles sea, underground
  • surveillance e.g., satellites, cluster satellites, etc.
  • FIG. 3 is a diagram illustrating an example of a system 300 for implementing some aspects of the subject technology.
  • the system 300 includes a processing system 302, which may include one or more processors or one or more processing systems.
  • a processor can be one or more processors.
  • the processing system 302 may include a general-purpose processor or a specific-purpose processor for executing instructions and may further include a machine- readable medium 319, such as a volatile or non-volatile memory, for storing data and/or instructions for software programs.
  • the instructions which may be stored in a machine-readable medium 310 and/or 319, may be executed by the processing system 302 to control and manage access to the various networks, as well as provide other communication and processing functions.
  • the instructions may also include instructions executed by the processing system 302 for various user interface devices, such as a display 312 and a keypad 314.
  • the processing system 302 may include an input port 322 and an output port 324.
  • Each of the input port 322 and the output port 324 may include one or more ports.
  • the input port 322 and the output port 324 may be the same port (e.g., a bi-directional port) or may be different ports.
  • the processing system 302 may be implemented using software, hardware, or a combination of both.
  • the processing system 302 may be implemented with one or more processors.
  • a processor may be a general-purpose microprocessor, a
  • DSP Digital Signal Processor
  • ASIC Application Specific Integrated Circuit
  • FPGA Field Programmable Gate Array
  • PLD Programmable Logic Device
  • controller a state machine, gated logic, discrete hardware components, or any other suitable device that can perform calculations or other manipulations of information.
  • a machine-readable medium can be one or more machine-readable media.
  • Software shall be construed broadly to mean instructions, data, or any combination thereof, whether referred to as software, firmware, middleware, microcode, hardware description language, or otherwise. Instructions may include code (e.g., in source code format, binary code format, executable code format, or any other suitable format of code).
  • Machine-readable media may include storage integrated into a processing system such as might be the case with an ASIC.
  • Machine-readable media may also include storage external to a processing system, such as a Random Access Memory (RAM), a flash memory, a Read Only Memory (ROM), a Programmable Read-Only Memory (PROM), an Erasable PROM (EPROM), registers, a hard disk, a removable disk, a CD-ROM, a DVD, or any other suitable storage device.
  • RAM Random Access Memory
  • ROM Read Only Memory
  • PROM Erasable PROM
  • registers a hard disk, a removable disk, a CD-ROM, a DVD, or any other suitable storage device.
  • a machine-readable medium is a computer-readable medium encoded or stored with instructions and is a computing element, which defines structural and functional interrelationships between the instructions and the rest of the system, which permit the instructions' functionality to be realized.
  • Instructions may be executable, for example, by the processing system 302 or one or more processors. Instructions can be, for example, a computer program including code for performing methods of the subject technology.
  • a network interface 316 may be any type of interface to a network (e.g., an Internet network interface), and may reside between any of the components shown in FIG. 3 and coupled to the processor via the bus 304.
  • a network e.g., an Internet network interface
  • a device interface 318 may be any type of interface to a device and may reside between any of the components shown in FIG. 3.
  • a device interface 318 may, for example, be an interface to an external device (e.g., USB device) that plugs into a port (e.g., USB port) of the system 300.
  • the device interface 318 may be the host interface of FIG. 1, where at least some of the functionalities of the apparatus of FIG. 1 are performed by the processing system 302.
  • One or more of the above-described features and applications may be implemented as software processes that are specified as a set of instructions recorded on a computer readable storage medium (alternatively referred to as computer-readable media, machine-readable media, or machine-readable storage media).
  • a computer readable storage medium alternatively referred to as computer-readable media, machine-readable media, or machine-readable storage media.
  • processing unit(s) e.g., one or more processors, cores of processors, or other processing units
  • the computer readable media does not include carrier waves and electronic signals passing wirelessly or over wired connections, or any other ephemeral signals.
  • the computer readable media may be entirely restricted to tangible, physical objects that store information in a form that is readable by a computer.
  • the computer readable media is non-transitory computer readable media, computer readable storage media, or non-transitory computer readable storage media.
  • a computer program product also known as a program, software, software application, script, or code
  • a computer program product can be written in any form of programming language, including compiled or interpreted languages, declarative or procedural languages, and it can be deployed in any form, including as a stand-alone program or as a module, component, subroutine, object, or other unit suitable for use in a computing
  • a computer program may, but need not, correspond to a file in a file system.
  • a program can be stored in a portion of a file that holds other programs or data (e.g., one or more scripts stored in a markup language document), in a single file dedicated to the program in question, or in multiple coordinated files (e.g., files that store one or more modules, sub programs, or portions of code).
  • a computer program can be deployed to be executed on one computer or on multiple computers that are located at one site or distributed across multiple sites and interconnected by a communication network.
  • ASICs application specific integrated circuits
  • FPGAs field programmable gate arrays
  • integrated circuits execute instructions that are stored on the circuit itself.
  • the subject technology is directed to method and systems for providing precisely timed laser actuation, RF waveform control, and synchronous acquisition of fluorescence information from a DNV magnetometer.
  • the subject technology may be used in various markets, including for example and without limitation, advanced sensors.

Landscapes

  • Physics & Mathematics (AREA)
  • Engineering & Computer Science (AREA)
  • General Physics & Mathematics (AREA)
  • Power Engineering (AREA)
  • Condensed Matter Physics & Semiconductors (AREA)
  • Automation & Control Theory (AREA)
  • Position Fixing By Use Of Radio Waves (AREA)

Abstract

L'invention concerne des systèmes, des contrôleurs et des configurations pour assurer un actionnement laser précisément cadencé, une commande de forme d'onde RF, et une acquisition synchrone d'informations de fluorescence à partir de composants de magnétométrie, tels qu'un capteur de lacunes d'azote de diamant (DNV). Un contrôleur pour un capteur DNV peut comprendre un générateur de forme d'onde RF pour générer une forme d'onde RF pour un signal RF pour un capteur DNV et une commande numérique pour commander un laser pour le capteur DNV. Le générateur de forme d'onde RF et la commande numérique peuvent être formés dans une même puce, telle qu'un FPGA ou ASIC.
PCT/US2016/014376 2016-01-21 2016-01-21 Contrôleur à jeu d'instructions réduit pour capteur de lacunes d'azote de diamant WO2017127091A1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US15/003,336 2016-01-21
US15/003,336 US20170212181A1 (en) 2016-01-21 2016-01-21 Reduced instruction set controller for diamond nitrogen vacancy sensor

Publications (1)

Publication Number Publication Date
WO2017127091A1 true WO2017127091A1 (fr) 2017-07-27

Family

ID=59359692

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/US2016/014376 WO2017127091A1 (fr) 2016-01-21 2016-01-21 Contrôleur à jeu d'instructions réduit pour capteur de lacunes d'azote de diamant

Country Status (2)

Country Link
US (1) US20170212181A1 (fr)
WO (1) WO2017127091A1 (fr)

Cited By (45)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9817081B2 (en) 2016-01-21 2017-11-14 Lockheed Martin Corporation Magnetometer with light pipe
US9823313B2 (en) 2016-01-21 2017-11-21 Lockheed Martin Corporation Diamond nitrogen vacancy sensor with circuitry on diamond
US9823381B2 (en) 2014-03-20 2017-11-21 Lockheed Martin Corporation Mapping and monitoring of hydraulic fractures using vector magnetometers
US9824597B2 (en) 2015-01-28 2017-11-21 Lockheed Martin Corporation Magnetic navigation methods and systems utilizing power grid and communication network
US9823314B2 (en) 2016-01-21 2017-11-21 Lockheed Martin Corporation Magnetometer with a light emitting diode
US9829545B2 (en) 2015-11-20 2017-11-28 Lockheed Martin Corporation Apparatus and method for hypersensitivity detection of magnetic field
US9835693B2 (en) 2016-01-21 2017-12-05 Lockheed Martin Corporation Higher magnetic sensitivity through fluorescence manipulation by phonon spectrum control
US9845153B2 (en) 2015-01-28 2017-12-19 Lockheed Martin Corporation In-situ power charging
US9853837B2 (en) 2014-04-07 2017-12-26 Lockheed Martin Corporation High bit-rate magnetic communication
US9910104B2 (en) 2015-01-23 2018-03-06 Lockheed Martin Corporation DNV magnetic field detector
US9910105B2 (en) 2014-03-20 2018-03-06 Lockheed Martin Corporation DNV magnetic field detector
US10006973B2 (en) 2016-01-21 2018-06-26 Lockheed Martin Corporation Magnetometer with a light emitting diode
US10012704B2 (en) 2015-11-04 2018-07-03 Lockheed Martin Corporation Magnetic low-pass filter
US10088336B2 (en) 2016-01-21 2018-10-02 Lockheed Martin Corporation Diamond nitrogen vacancy sensed ferro-fluid hydrophone
US10088452B2 (en) 2016-01-12 2018-10-02 Lockheed Martin Corporation Method for detecting defects in conductive materials based on differences in magnetic field characteristics measured along the conductive materials
US10120039B2 (en) 2015-11-20 2018-11-06 Lockheed Martin Corporation Apparatus and method for closed loop processing for a magnetic detection system
US10126377B2 (en) 2016-05-31 2018-11-13 Lockheed Martin Corporation Magneto-optical defect center magnetometer
US10145910B2 (en) 2017-03-24 2018-12-04 Lockheed Martin Corporation Photodetector circuit saturation mitigation for magneto-optical high intensity pulses
US10168393B2 (en) 2014-09-25 2019-01-01 Lockheed Martin Corporation Micro-vacancy center device
US10228429B2 (en) 2017-03-24 2019-03-12 Lockheed Martin Corporation Apparatus and method for resonance magneto-optical defect center material pulsed mode referencing
US10241158B2 (en) 2015-02-04 2019-03-26 Lockheed Martin Corporation Apparatus and method for estimating absolute axes' orientations for a magnetic detection system
US10277208B2 (en) 2014-04-07 2019-04-30 Lockheed Martin Corporation Energy efficient controlled magnetic field generator circuit
US10274550B2 (en) 2017-03-24 2019-04-30 Lockheed Martin Corporation High speed sequential cancellation for pulsed mode
US10281550B2 (en) 2016-11-14 2019-05-07 Lockheed Martin Corporation Spin relaxometry based molecular sequencing
US10317279B2 (en) 2016-05-31 2019-06-11 Lockheed Martin Corporation Optical filtration system for diamond material with nitrogen vacancy centers
US10333588B2 (en) 2015-12-01 2019-06-25 Lockheed Martin Corporation Communication via a magnio
US10330744B2 (en) 2017-03-24 2019-06-25 Lockheed Martin Corporation Magnetometer with a waveguide
US10338163B2 (en) 2016-07-11 2019-07-02 Lockheed Martin Corporation Multi-frequency excitation schemes for high sensitivity magnetometry measurement with drift error compensation
US10338162B2 (en) 2016-01-21 2019-07-02 Lockheed Martin Corporation AC vector magnetic anomaly detection with diamond nitrogen vacancies
US10338164B2 (en) 2017-03-24 2019-07-02 Lockheed Martin Corporation Vacancy center material with highly efficient RF excitation
US10345396B2 (en) 2016-05-31 2019-07-09 Lockheed Martin Corporation Selected volume continuous illumination magnetometer
US10345395B2 (en) 2016-12-12 2019-07-09 Lockheed Martin Corporation Vector magnetometry localization of subsurface liquids
US10359479B2 (en) 2017-02-20 2019-07-23 Lockheed Martin Corporation Efficient thermal drift compensation in DNV vector magnetometry
US10371765B2 (en) 2016-07-11 2019-08-06 Lockheed Martin Corporation Geolocation of magnetic sources using vector magnetometer sensors
US10371760B2 (en) 2017-03-24 2019-08-06 Lockheed Martin Corporation Standing-wave radio frequency exciter
US10379174B2 (en) 2017-03-24 2019-08-13 Lockheed Martin Corporation Bias magnet array for magnetometer
US10408890B2 (en) 2017-03-24 2019-09-10 Lockheed Martin Corporation Pulsed RF methods for optimization of CW measurements
US10408889B2 (en) 2015-02-04 2019-09-10 Lockheed Martin Corporation Apparatus and method for recovery of three dimensional magnetic field from a magnetic detection system
US10459041B2 (en) 2017-03-24 2019-10-29 Lockheed Martin Corporation Magnetic detection system with highly integrated diamond nitrogen vacancy sensor
US10466312B2 (en) 2015-01-23 2019-11-05 Lockheed Martin Corporation Methods for detecting a magnetic field acting on a magneto-optical detect center having pulsed excitation
CN110543118A (zh) * 2019-08-28 2019-12-06 桂林电子科技大学 一种带触发监控的通用fpga同步触发控制器及方法
US10520558B2 (en) 2016-01-21 2019-12-31 Lockheed Martin Corporation Diamond nitrogen vacancy sensor with nitrogen-vacancy center diamond located between dual RF sources
US10527746B2 (en) 2016-05-31 2020-01-07 Lockheed Martin Corporation Array of UAVS with magnetometers
US10571530B2 (en) 2016-05-31 2020-02-25 Lockheed Martin Corporation Buoy array of magnetometers
US10677953B2 (en) 2016-05-31 2020-06-09 Lockheed Martin Corporation Magneto-optical detecting apparatus and methods

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102019128932A1 (de) 2019-10-25 2021-04-29 Carl Zeiss Ag Verfahren, Vorrichtungen und System zum Messen einer Messgröße

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5245347A (en) * 1980-12-29 1993-09-14 Raytheon Company All weather tactical strike system (AWTSS) and method of operation
US20030058346A1 (en) * 1997-04-02 2003-03-27 Bechtel Jon H. Control circuit for image array sensors
US20140340085A1 (en) * 2013-05-17 2014-11-20 Massachusetts Institute Of Technology Time-resolved magnetic sensing with electronic spins in diamond
WO2014210486A1 (fr) * 2013-06-28 2014-12-31 Dirk Robert Englund Détection à large champ au moyen de lacunes d'azote
US20150192532A1 (en) * 2014-01-08 2015-07-09 Massachusetts Institute Of Technology Methods and apparatus for optically detecting magnetic resonance

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5245347A (en) * 1980-12-29 1993-09-14 Raytheon Company All weather tactical strike system (AWTSS) and method of operation
US20030058346A1 (en) * 1997-04-02 2003-03-27 Bechtel Jon H. Control circuit for image array sensors
US20140340085A1 (en) * 2013-05-17 2014-11-20 Massachusetts Institute Of Technology Time-resolved magnetic sensing with electronic spins in diamond
WO2014210486A1 (fr) * 2013-06-28 2014-12-31 Dirk Robert Englund Détection à large champ au moyen de lacunes d'azote
US20150192532A1 (en) * 2014-01-08 2015-07-09 Massachusetts Institute Of Technology Methods and apparatus for optically detecting magnetic resonance

Cited By (48)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10725124B2 (en) 2014-03-20 2020-07-28 Lockheed Martin Corporation DNV magnetic field detector
US9823381B2 (en) 2014-03-20 2017-11-21 Lockheed Martin Corporation Mapping and monitoring of hydraulic fractures using vector magnetometers
US9910105B2 (en) 2014-03-20 2018-03-06 Lockheed Martin Corporation DNV magnetic field detector
US9853837B2 (en) 2014-04-07 2017-12-26 Lockheed Martin Corporation High bit-rate magnetic communication
US10277208B2 (en) 2014-04-07 2019-04-30 Lockheed Martin Corporation Energy efficient controlled magnetic field generator circuit
US10168393B2 (en) 2014-09-25 2019-01-01 Lockheed Martin Corporation Micro-vacancy center device
US10466312B2 (en) 2015-01-23 2019-11-05 Lockheed Martin Corporation Methods for detecting a magnetic field acting on a magneto-optical detect center having pulsed excitation
US9910104B2 (en) 2015-01-23 2018-03-06 Lockheed Martin Corporation DNV magnetic field detector
US9824597B2 (en) 2015-01-28 2017-11-21 Lockheed Martin Corporation Magnetic navigation methods and systems utilizing power grid and communication network
US9845153B2 (en) 2015-01-28 2017-12-19 Lockheed Martin Corporation In-situ power charging
US10241158B2 (en) 2015-02-04 2019-03-26 Lockheed Martin Corporation Apparatus and method for estimating absolute axes' orientations for a magnetic detection system
US10408889B2 (en) 2015-02-04 2019-09-10 Lockheed Martin Corporation Apparatus and method for recovery of three dimensional magnetic field from a magnetic detection system
US10012704B2 (en) 2015-11-04 2018-07-03 Lockheed Martin Corporation Magnetic low-pass filter
US10120039B2 (en) 2015-11-20 2018-11-06 Lockheed Martin Corporation Apparatus and method for closed loop processing for a magnetic detection system
US9829545B2 (en) 2015-11-20 2017-11-28 Lockheed Martin Corporation Apparatus and method for hypersensitivity detection of magnetic field
US10333588B2 (en) 2015-12-01 2019-06-25 Lockheed Martin Corporation Communication via a magnio
US10088452B2 (en) 2016-01-12 2018-10-02 Lockheed Martin Corporation Method for detecting defects in conductive materials based on differences in magnetic field characteristics measured along the conductive materials
US9817081B2 (en) 2016-01-21 2017-11-14 Lockheed Martin Corporation Magnetometer with light pipe
US10338162B2 (en) 2016-01-21 2019-07-02 Lockheed Martin Corporation AC vector magnetic anomaly detection with diamond nitrogen vacancies
US9835694B2 (en) 2016-01-21 2017-12-05 Lockheed Martin Corporation Higher magnetic sensitivity through fluorescence manipulation by phonon spectrum control
US9823313B2 (en) 2016-01-21 2017-11-21 Lockheed Martin Corporation Diamond nitrogen vacancy sensor with circuitry on diamond
US9835693B2 (en) 2016-01-21 2017-12-05 Lockheed Martin Corporation Higher magnetic sensitivity through fluorescence manipulation by phonon spectrum control
US10006973B2 (en) 2016-01-21 2018-06-26 Lockheed Martin Corporation Magnetometer with a light emitting diode
US9823314B2 (en) 2016-01-21 2017-11-21 Lockheed Martin Corporation Magnetometer with a light emitting diode
US10088336B2 (en) 2016-01-21 2018-10-02 Lockheed Martin Corporation Diamond nitrogen vacancy sensed ferro-fluid hydrophone
US10520558B2 (en) 2016-01-21 2019-12-31 Lockheed Martin Corporation Diamond nitrogen vacancy sensor with nitrogen-vacancy center diamond located between dual RF sources
US10126377B2 (en) 2016-05-31 2018-11-13 Lockheed Martin Corporation Magneto-optical defect center magnetometer
US10527746B2 (en) 2016-05-31 2020-01-07 Lockheed Martin Corporation Array of UAVS with magnetometers
US10317279B2 (en) 2016-05-31 2019-06-11 Lockheed Martin Corporation Optical filtration system for diamond material with nitrogen vacancy centers
US10345396B2 (en) 2016-05-31 2019-07-09 Lockheed Martin Corporation Selected volume continuous illumination magnetometer
US10571530B2 (en) 2016-05-31 2020-02-25 Lockheed Martin Corporation Buoy array of magnetometers
US10677953B2 (en) 2016-05-31 2020-06-09 Lockheed Martin Corporation Magneto-optical detecting apparatus and methods
US10338163B2 (en) 2016-07-11 2019-07-02 Lockheed Martin Corporation Multi-frequency excitation schemes for high sensitivity magnetometry measurement with drift error compensation
US10371765B2 (en) 2016-07-11 2019-08-06 Lockheed Martin Corporation Geolocation of magnetic sources using vector magnetometer sensors
US10281550B2 (en) 2016-11-14 2019-05-07 Lockheed Martin Corporation Spin relaxometry based molecular sequencing
US10345395B2 (en) 2016-12-12 2019-07-09 Lockheed Martin Corporation Vector magnetometry localization of subsurface liquids
US10359479B2 (en) 2017-02-20 2019-07-23 Lockheed Martin Corporation Efficient thermal drift compensation in DNV vector magnetometry
US10274550B2 (en) 2017-03-24 2019-04-30 Lockheed Martin Corporation High speed sequential cancellation for pulsed mode
US10408890B2 (en) 2017-03-24 2019-09-10 Lockheed Martin Corporation Pulsed RF methods for optimization of CW measurements
US10459041B2 (en) 2017-03-24 2019-10-29 Lockheed Martin Corporation Magnetic detection system with highly integrated diamond nitrogen vacancy sensor
US10379174B2 (en) 2017-03-24 2019-08-13 Lockheed Martin Corporation Bias magnet array for magnetometer
US10338164B2 (en) 2017-03-24 2019-07-02 Lockheed Martin Corporation Vacancy center material with highly efficient RF excitation
US10330744B2 (en) 2017-03-24 2019-06-25 Lockheed Martin Corporation Magnetometer with a waveguide
US10371760B2 (en) 2017-03-24 2019-08-06 Lockheed Martin Corporation Standing-wave radio frequency exciter
US10228429B2 (en) 2017-03-24 2019-03-12 Lockheed Martin Corporation Apparatus and method for resonance magneto-optical defect center material pulsed mode referencing
US10145910B2 (en) 2017-03-24 2018-12-04 Lockheed Martin Corporation Photodetector circuit saturation mitigation for magneto-optical high intensity pulses
CN110543118A (zh) * 2019-08-28 2019-12-06 桂林电子科技大学 一种带触发监控的通用fpga同步触发控制器及方法
CN110543118B (zh) * 2019-08-28 2020-11-13 桂林电子科技大学 一种带触发监控的通用fpga同步触发控制器及方法

Also Published As

Publication number Publication date
US20170212181A1 (en) 2017-07-27

Similar Documents

Publication Publication Date Title
US20170212181A1 (en) Reduced instruction set controller for diamond nitrogen vacancy sensor
US10241197B2 (en) Method of preparing histograms of a sensor signal from an array of sensors, in particular proximity sensors, and corresponding device
CN105549006A (zh) 一种基于fpga&soc手持式探地雷达系统
US10101439B2 (en) Apparatus and method for controlling power of vehicle radar
US10249781B2 (en) Apparatus for counting single photons and method thereof
JP6453068B2 (ja) 磁気共鳴イメージング装置
JP6278777B2 (ja) レーダ電波識別装置、レーダ電波識別方法及びプログラム
WO2016046696A3 (fr) Bobine de récepteur numérique dotée d'un indicateur de bruit de phase reçue intégré
CN103344228B (zh) 摇动质量体声波固体波动微陀螺驱动与检测电路
RU2012100936A (ru) Корреляционный измеритель высоты и составляющих вектора путевой скорости
CN105806198B (zh) 异步输出协议
CN103180758B (zh) 用于金属探测系统的方法及装置
KR102062321B1 (ko) 대상체의 동작을 인식하기 위하여 복수개의 상이한 주파수들을 이용하는 센서 모듈 및 그 센서 모듈의 동작 방법
CN105352627A (zh) 一种温度检测系统及其检测方法
CN110988760B (zh) 一种Mx型铯光泵磁力仪的数字化信号检测系统
US10794994B2 (en) Radar control device and method of controlling transmission power of radar
RU2016151766A (ru) Удельная скорость поглощения, модулируемая пространственной близостью к пациенту
CN1924607B (zh) 多工作状态的高频雷达接收机的控制方法
CN102944784A (zh) 一种mri梯度线圈涡流测量装置及方法
KR101971722B1 (ko) 동기화된 위성항법 시스템 기만신호 생성 장치 및 그 방법
US20170212216A1 (en) Measuring device and measuring method for measuring the ambiguity function of radar signals
Liu et al. Signal acquisition technology for photoelectric encoder based on FPGA
CN202196163U (zh) 一种基于PXI/PXIe总线的数字化磁共振成像谱仪
Tokmachev et al. A synchronization system of very low-frequency interferometers
CN205157648U (zh) 一种无盲区数字相位计装置

Legal Events

Date Code Title Description
121 Ep: the epo has been informed by wipo that ep was designated in this application

Ref document number: 16886729

Country of ref document: EP

Kind code of ref document: A1

NENP Non-entry into the national phase

Ref country code: DE

122 Ep: pct application non-entry in european phase

Ref document number: 16886729

Country of ref document: EP

Kind code of ref document: A1